Sodemo V2-1.2
{{Short description|French aircraft engine}}
{{Use dmy dates|date=January 2022}}
{{Use British English|date=January 2022}}
| {{Infobox aircraft begin
| name=V2-1.2 | image= | caption= }}{{Infobox Aircraft Engine |type=Aircraft engine |manufacturer=Sodemo |designer= |national origin=France |first run= |major applications= |produced= |number built= |developed from= |variants with their own articles= }} |
The Sodemo V2-1.2 is a French aircraft engine, designed and produced by Sodemo of Magny-Cours, for use in light aircraft.Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 256-257. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}
Design and development
The engine is a 90° V-twin-cylinder four-stroke, {{convert|1200|cc|cuin|1|abbr=on}} displacement, liquid-cooled, petrol engine design, with a mechanical helical-gear gearbox reduction drive. It employs dual capacitor discharge ignition and produces {{convert|136|hp|kW|0|abbr=on}}.
Specifications (V2-1.2)
{{pistonspecs|
|type=Twin cylinder, four stroke aircraft engine
|bore=
|stroke=
|displacement={{convert|992|cc|cuin|1|abbr=on}}
|length=
|diameter=
|width=
|height=
|weight=
|valvetrain=
|supercharger=
|turbocharger=
|fuelsystem=
|fueltype=petrol
|oilsystem=
|coolingsystem=liquid
|power={{convert|136|hp|kW|0|abbr=on}}
|specpower=
|compression=
|fuelcon=
|specfuelcon=
|oilcon=
|power/weight=
|designer=
|reduction_gear=
|general_other=
|components_other=
|performance_other=
}}
See also
{{aircontent
|see also=
|related=*Sodemo V2-1.0
|similar aircraft=
|lists= *List of aircraft engines
}}
References
{{Reflist}}
External links
- {{Official website|http://www.sodemo.com/en/14/the-v2-engine.html}}
Category:Sodemo aircraft engines